GB0614894D0 - Integrally Bladed Rotor - Google Patents

Integrally Bladed Rotor

Info

Publication number
GB0614894D0
GB0614894D0 GBGB0614894.4A GB0614894A GB0614894D0 GB 0614894 D0 GB0614894 D0 GB 0614894D0 GB 0614894 A GB0614894 A GB 0614894A GB 0614894 D0 GB0614894 D0 GB 0614894D0
Authority
GB
United Kingdom
Prior art keywords
bladed rotor
integrally bladed
integrally
rotor
bladed
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
GBGB0614894.4A
Other versions
GB2440345A (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB0614894A priority Critical patent/GB2440345A/en
Publication of GB0614894D0 publication Critical patent/GB0614894D0/en
Publication of GB2440345A publication Critical patent/GB2440345A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Architecture (AREA)
  • Ceramic Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB0614894A 2006-07-26 2006-07-26 Integrally bladed rotor having blades made of metallic and non-metallic materials Withdrawn GB2440345A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0614894A GB2440345A (en) 2006-07-26 2006-07-26 Integrally bladed rotor having blades made of metallic and non-metallic materials

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0614894A GB2440345A (en) 2006-07-26 2006-07-26 Integrally bladed rotor having blades made of metallic and non-metallic materials

Publications (2)

Publication Number Publication Date
GB0614894D0 true GB0614894D0 (en) 2006-09-06
GB2440345A GB2440345A (en) 2008-01-30

Family

ID=37006232

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0614894A Withdrawn GB2440345A (en) 2006-07-26 2006-07-26 Integrally bladed rotor having blades made of metallic and non-metallic materials

Country Status (1)

Country Link
GB (1) GB2440345A (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8844265B2 (en) 2007-08-01 2014-09-30 United Technologies Corporation Turbine section of high bypass turbofan
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US20150377123A1 (en) 2007-08-01 2015-12-31 United Technologies Corporation Turbine section of high bypass turbofan
US11149650B2 (en) 2007-08-01 2021-10-19 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11242805B2 (en) 2007-08-01 2022-02-08 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
DE102009052880A1 (en) * 2009-11-13 2011-05-19 Mtu Aero Engines Gmbh Method for producing an integrally bladed rotor, device for carrying out the method and rotor produced by the method
FR2956599B1 (en) * 2010-02-22 2012-04-27 Snecma PROCESS FOR PRODUCING A MONOBLOC AUBAGE RING
FR2970943B1 (en) 2011-01-31 2014-02-28 Eurocopter France BLADE AND METHOD FOR MANUFACTURING THE SAME
EP2959110B1 (en) * 2013-02-23 2017-06-28 Rolls-Royce Corporation Gas turbine engine component
US8869504B1 (en) 2013-11-22 2014-10-28 United Technologies Corporation Geared turbofan engine gearbox arrangement
FR3027340B1 (en) * 2014-10-15 2019-06-21 Safran Aircraft Engines MONOBLOC DRAWING DISK HAVING A HUB PROVIDED WITH RADIAL SLOTS DELIMINATING BLADE PADS
GB2560001B (en) * 2017-02-24 2019-07-17 Rolls Royce Plc A weld stub arrangement and a method of using the arrangement to make an article

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1040825A (en) * 1965-04-20 1966-09-01 Rolls Royce Improvements in rotor blades and/or stator blades for gas turbine engines
FR2723868B1 (en) * 1994-08-24 1996-09-20 Snecma PROCESS FOR OBTAINING A METAL CIRCULAR PIECE WITH BLADES
DE19751129C1 (en) * 1997-11-19 1999-06-17 Mtu Muenchen Gmbh FAN rotor blade for an engine
US6190133B1 (en) * 1998-08-14 2001-02-20 Allison Engine Company High stiffness airoil and method of manufacture
US6544003B1 (en) * 2000-11-08 2003-04-08 General Electric Co. Gas turbine blisk with ceramic foam blades and its preparation

Also Published As

Publication number Publication date
GB2440345A (en) 2008-01-30

Similar Documents

Publication Publication Date Title
GB0724612D0 (en) Rotor blades
GB0614894D0 (en) Integrally Bladed Rotor
PL2010757T3 (en) Turbine blade
EP2031732A4 (en) Motor rotor
GB2450936B (en) Bladed rotor balancing
GB2426297B (en) Turbine / rotor
GB0524735D0 (en) Turbine blade
GB0600532D0 (en) A blade and rotor arrangement
GB2451568B (en) Rotor blade
GB2448886B (en) Turbomachine blade
EP2019186A4 (en) Blade
GB0613441D0 (en) Blades
GB0715509D0 (en) Rotor
PL2032803T3 (en) Rotor with cut-outs
GB0602065D0 (en) Turbine Blade
GB2443252B (en) Blade
EP2057732A4 (en) Outer rotor type fan-motor
GB2440614B (en) Turbomachine blade
GB0604508D0 (en) Turbine blade arrangement
GB0612993D0 (en) Centrifugal impeller
GB2460021B (en) Rotor blades
GB2438492B (en) Blades
GB0614186D0 (en) Blades
EP2123862A4 (en) Turbine blade
SI1818543T1 (en) Blade for impeller

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)